View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 48277U 26145.06001947 +.00000000 +00000-0 +12446-2 0 00005
2 48277 53.1262 17.7217 0005122 111.3002 248.8545 15.29647716 06
| Epoch (UTC): | 25 May 2026 01:26:25 |
| Eccentricity: | 0.0005122 |
| inclination: | 53.1262° |
| perigee height: | 473 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 17.7217° |
| argument of perigee: | 111.3002° |
| revolutions per day: | 15.29647716 |
| mean anomaly at epoch: | 248.8545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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